Chapter 4, Fluid Kinematics
To study the fluid motion without the consideration of the forces necessary to produce the motion
1. Velocity Field
V = u(x,y,z,t)i + vj + wk
|V| =(u2 + v2 + w2)1/2
i) Description
Langrangian flow description: following the individual fluid particles (Closed System)
Eulerian flow description: obtaining information about the flow in terms of what happen at fixed points in space as the flow past these points (Control Volume)
ii) Fluid flow is generally three-dimensional
V = u(x,y,z,t)i + vj + wk
It may be simplified to
one-dimensional, V = u(x,t)i Pipe flow
two-dimensional, V = u(x,t)i + v(y,t)j around a cylinder
iii) Unsteady and Turbulent
Assume steady ∂V/∂t = 0
laminar Re < 2300 for pipe flows
2. The Acceleration Field
Velocity
V = u(x,y,z,t)i + vj + wk
Acceleration
a = dV/dt = ∂V/∂t + (∂V/∂x)(dx/dt) + (∂V/∂y)(dy/dt)
+ (∂V/∂z)(dz/dt)
Since u = dx/dt, v = dy/dt, w = dz/dt
i) Material derivative
a = DV/Dt
= ∂V/∂t + u(∂V/∂x) + v(∂V/∂y) + w(∂V/∂z)
= ∂V/∂t + V∙V
where the vector operator,
del = = i∂/∂x + j∂/∂y + k∂/∂z
3. Control Volume and System Representation
System: consider all mass as the system (Lagrangian)
Control Volume: consider a space through which mass may flow in and out (Eulerian)
4. Reynolds Transport Theorem
At time t, Sys(t) = CV(t)
At time t = δt,
Sys (t+δt) = [(CV -I) + II](t+δt)
Let B = the extensive property
B = mb = ∫ ρbdV
Bsys(t+δt) = BCV(t+δt) - BI(t+δt) +BII(t+δt)
δBsys(t+δt)/δt = [Bsys(t+δt) - Bsys(t)]/δt
= [BCV(t+δt) - BCV(t)]/δt - BI(t+δt)/δt + BII(t+δt)/δt
As δt 0, Reynolds Transport Theorem
DBsys/Dt = ∂BCV/∂t - Bin + Bout
= (∂/∂t)∫ bρdV + ∫ bρV∙ndA
CV CS
In one-dimensional flow
DBsys/Dt = ∂BCV/∂t + [(ρAVb)out - (ρAVb)in]CS